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CN106050466A - Piston ring for internal combustion engines - Google Patents

Piston ring for internal combustion engines Download PDF

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Publication number
CN106050466A
CN106050466A CN201610235623.6A CN201610235623A CN106050466A CN 106050466 A CN106050466 A CN 106050466A CN 201610235623 A CN201610235623 A CN 201610235623A CN 106050466 A CN106050466 A CN 106050466A
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coating
outer layer
piston ring
chromium
thickness
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CN106050466B (en
Inventor
茹利亚诺·阿韦拉尔·阿劳霍
保罗·若泽·达·罗沙·莫尔登特
罗伯特·理查德·班菲尔德
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Mahle Metal Leve SA
Mahle International GmbH
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Mahle Metal Leve SA
Mahle International GmbH
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J9/00Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
    • F16J9/26Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction characterised by the use of particular materials
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/0021Reactive sputtering or evaporation
    • C23C14/0036Reactive sputtering
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/02Pretreatment of the material to be coated
    • C23C14/021Cleaning or etching treatments
    • C23C14/022Cleaning or etching treatments by means of bombardment with energetic particles or radiation
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0641Nitrides
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14Metallic material, boron or silicon
    • C23C14/16Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
    • C23C14/165Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon by cathodic sputtering
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/34Sputtering
    • C23C14/3485Sputtering using pulsed power to the target
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/34Sputtering
    • C23C14/35Sputtering by application of a magnetic field, e.g. magnetron sputtering
    • C23C14/352Sputtering by application of a magnetic field, e.g. magnetron sputtering using more than one target
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J9/00Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
    • F16J9/12Details

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Physical Vapour Deposition (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)

Abstract

本发明涉及用于内燃机的活塞环(1),设置有基本上环形的铁合金的基体(2),所述基体(2)上涂覆有包括第一结合层(10)和至少第一外层(11)或第二外层(12)的涂层(4),所述第一外层(11)和所述第二外层(12)沉积在所述第一结合层(10)上,多个相继沉积的第一和第二外层(11,12)达到最大100微米的厚度,从而由于涂层与基体的高粘和性、低内应力、高硬度以及低孔隙率而在活塞环(1)上提供出色的耐磨性。

The invention relates to a piston ring (1) for an internal combustion engine, provided with a substantially annular base body (2) of a ferrous alloy, said base body (2) being coated with a coating comprising a first bonding layer (10) and at least a first outer layer (11) or a coating (4) of a second outer layer (12), said first outer layer (11) and said second outer layer (12) being deposited on said first bonding layer (10), A plurality of successively deposited first and second outer layers (11, 12) up to a thickness of up to 100 micrometers, so that due to the high adhesion of the coating to the substrate, low internal stress, high hardness and low porosity in the piston ring (1) provides excellent wear resistance.

Description

用于内燃机的活塞环Piston rings for internal combustion engines

技术领域technical field

本发明涉及用于内燃机的活塞环,其中至少活塞环的基体设置有由氮化物组成的多层涂层,所述涂层通过物理气相沉积的工序涂覆并且由于涂层与基体的高粘和性、低内应力、高硬度以及低孔隙率而提供出色的耐磨性。The invention relates to piston rings for internal combustion engines, in which at least the base body of the piston ring is provided with a multilayer coating composed of nitrides, which is applied by the process of physical vapor deposition and due to the high adhesion of the coating to the base body Excellent wear resistance due to high hardness, low internal stress, high hardness and low porosity.

背景技术Background technique

内燃机基本上由两个主要部分组成:发动机机体(设置有一个或多个气缸)以及曲柄轴组件或者连接有一个或多个盖的曲柄轴组件。曲柄轴组件包含活塞、连接杆以及曲柄轴,该组件负责活塞在发动机机体的气缸内的位移。活塞为气缸的一部分,作为一种规则由金属基体组成,并且包括一个或多个环,所述环负责在活塞的外边缘与气缸的内壁之间提供滑动密封。An internal combustion engine basically consists of two main parts: the engine block (provided with one or more cylinders) and the crankshaft assembly or crankshaft assembly to which one or more heads are attached. The crankshaft assembly contains the pistons, connecting rods, and crankshaft, and is responsible for the displacement of the pistons within the cylinders of the engine block. The piston is part of the cylinder, consisting as a rule of a metallic matrix and comprising one or more rings responsible for providing a sliding seal between the outer edge of the piston and the inner wall of the cylinder.

作为一种规则,更多的当代四冲程发动机在每个活塞上利用三个环,两个压缩环和一个油环。两个最靠近活塞头定位的环被命名为压缩环并且用于在活塞进行压缩运动时防止气体混合物泄漏至曲柄箱的内部。活塞的第三个环被命名为油环并且具有从气缸壁刮过多的油的目的,从而控制油膜的厚度。As a rule, more contemporary four-stroke engines utilize three rings on each piston, two compression rings and one oil ring. The two rings located closest to the piston head are named compression rings and serve to prevent leakage of the gas mixture into the interior of the crankcase when the piston performs a compression movement. The third ring of the piston is named the oil ring and has the purpose of scraping excess oil from the cylinder wall, thereby controlling the thickness of the oil film.

通常,活塞环由金属外部基体形成,所述金属外部基体涂覆有至少一层适于与气缸壁接触的涂层。由于力图赋予环低滑动摩擦、高耐磨性、硬度和韧性的特性的事实,所以涂层的功能是非常重要的。Typically, piston rings are formed from a metallic outer substrate coated with at least one coating suitable for contact with the cylinder wall. The function of the coating is very important due to the fact that one seeks to impart to the ring the properties of low sliding friction, high wear resistance, hardness and toughness.

作为一种规则,涂层的涂覆通过离子镀膜工序进行,特别是物理气相沉积(PVD)、化学气相沉积(CVD)或者通过电镀工序进行。As a rule, the coating is applied by ion-plating processes, in particular physical vapor deposition (PVD), chemical vapor deposition (CVD) or by electroplating processes.

在用于涂覆活塞环的工序中,物理气相沉积(PVD)工序体现了令人感兴趣的益处,例如,工序以非常低的工作压力操作的可能性、为高纯度材料的烧结提供可行性、由于通过离子撞击而“清洁”基体的表面的可能性而提高涂层与基体的粘和性;统一的涂层厚度、涂层的晶体结构的控制、因在多数情况中不涉及有毒产品或者溶液并且沉积温度相对低的事实,无论如何不会使用污水或污染物。Among the processes used to coat piston rings, the Physical Vapor Deposition (PVD) process presents interesting benefits, such as the possibility of the process operating at very low operating pressures, the possibility of sintering of high-purity materials , increased adhesion of the coating to the substrate due to the possibility of "cleaning" the surface of the substrate by ion impact; uniform coating thickness, control of the crystal structure of the coating, since in most cases no toxic products or solution and the fact that the deposition temperature is relatively low, no sewage or pollutants will be used anyway.

用于物理气相沉积(PVD)的基本工序已知为蒸镀和溅镀。阴极电弧(蒸镀)产生目标阴极的粗略的微熔化,从而对液体的液滴或大粒子(在阴极电弧工序中产生的液体颗粒或者固体碎片)进行溅镀。这些大粒子可以改变尺寸至大约100纳米,这些大粒子的平均直径在5纳米和30纳米之间,并且影响涂层的诸如摩擦、耐磨性、耐腐蚀性、电阻率以及反射率的许多特性。The basic procedures for physical vapor deposition (PVD) are known as evaporation and sputtering. Cathodic arcing (evaporation) produces a rough micro-melting of the target cathode, thereby sputtering droplets of liquid or large particles (liquid particles or solid fragments produced in the cathodic arcing process). These macroparticles can change in size up to about 100 nanometers, the average diameter of these macroparticles is between 5 nanometers and 30 nanometers, and affect many properties of the coating such as friction, wear resistance, corrosion resistance, electrical resistivity, and reflectivity .

耐腐蚀性,例如,在大粒子合并到涂层中时被折中,有可能被认为在密集和连续的涂层中中断。作为一种规则,考虑工作的一个可能的过程而使用过滤,然而这些过滤减少了沉积率并且增加了复杂性和设备成本。Corrosion resistance, for example, is compromised when large particles are incorporated into the coating, likely to be considered interrupted in dense and continuous coatings. As a rule, filters are used considering a possible course of work, however these filters reduce deposition rates and increase complexity and equipment costs.

PVD溅镀过程是涉及从源头喷射原子或分子的不加热汽化。该技术的演化,例如,高功率脉冲磁控溅镀(HiPIMS)方法,为获得缺少密集的大粒子的涂层提供可能性,从而为其应用至活塞环提供可行性。The PVD sputtering process is an unheated vaporization involving the ejection of atoms or molecules from a source. Evolution of this technology, for example the High Power Pulsed Magnetron Sputtering (HiPIMS) method, offers the possibility to obtain coatings devoid of dense macroparticles, thus enabling their application to piston rings.

在目前,现有技术的活塞环设置有外部基体或者滑动基体,所述外部基体或者滑动基体设置有氮化铬(CrN)的单层涂层,从而提供耐磨性。该涂层由阴极电弧PVD工序获得。At present, prior art piston rings are provided with an outer matrix or sliding matrix provided with a single layer coating of chromium nitride (CrN) to provide wear resistance. The coating is obtained by a cathodic arc PVD process.

当用于具有高负荷和高燃烧压力水平的发动机中时,该涂层呈现出脆弱的性能,导致由于高内应力在活塞环的基体中出现细微裂缝。这些细微裂缝传播,导致涂层的小片的脱落,在基体中产生空白,并且甚至可能使气缸衬套的表面出现伤痕。When used in engines with high loads and high combustion pressure levels, the coating exhibits fragile properties, resulting in the appearance of microcracks in the matrix of the piston rings due to high internal stresses. These microcracks propagate, causing flakes of the coating to flake off, creating voids in the substrate, and may even scar the surface of the cylinder liner.

而且,除了产生粗糙的表面并且导致滑动基体的孔隙率降低这些对于活塞环涂层而言不期望的效果,如上所述,存在形成大粒子的可能性,具有导致基体上的涂层的粘和性损失的可能性。Moreover, in addition to the undesired effects for piston ring coatings of creating a rough surface and resulting in a reduced porosity of the sliding substrate, as mentioned above, there is the possibility of forming large particles, with the potential to cause sticking of the coating on the substrate. Possibility of sexual loss.

与本发明具有相同的所有权人的现有技术文献PI 1102335-0以及PI1102336-8揭露了用于在设置有用于内燃机的滑动表面的元件上获得单层涂层的高功率脉冲磁控溅镀(HiPIMS)工序。这样的沉积工序除了低内应力还赋予高耐磨性。Prior art documents PI 1102335-0 and PI 1102336-8 of the same ownership as the present invention disclose high power pulsed magnetron sputtering ( HiPIMS) process. Such a deposition procedure imparts high wear resistance in addition to low internal stress.

应当注意的是,现有技术中出现的涂层为单层型,也就是说只有一个沉积层。根据沉积工序,单层涂层呈现出或多或少的耐磨性,然而没有呈现出足够的强度而且没有呈现出适于应用在高负荷发动机的活塞上。It should be noted that the coatings presented in the prior art are of the monolayer type, that is to say there is only one deposited layer. Depending on the deposition procedure, the single-layer coating exhibits more or less wear resistance, but does not exhibit sufficient strength and does not appear to be suitable for application on pistons of highly loaded engines.

因此,需要提供活塞环的获得,其中至少活塞环的基体设置有由氮化物组成的多层涂层,所述涂层由于涂层与基体的高粘和性、低内应力、高硬度以及低孔隙率而提供出色的耐磨性。Therefore, there is a need to provide piston rings in which at least the base body of the piston ring is provided with a multilayer coating composed of nitrides, which due to the high adhesion of the coating to the base body, low internal stress, high hardness and low Excellent wear resistance due to porosity.

发明内容Contents of the invention

发明目的purpose of invention

本发明的目的是提供一种活塞环,所述活塞环包括设置有由于涂层与基体的高粘和性、低内应力、高硬度以及低孔隙率而确保出色的耐磨性的多层涂层的基体。The object of the present invention is to provide a piston ring comprising a multilayer coating which ensures excellent wear resistance due to high adhesion of the coating to the substrate, low internal stress, high hardness and low porosity. layer base.

本发明另外的目的是提供一种活塞环,所述活塞环包括基体,所述基体设置有由金属氮化物组成的涂层,所述涂层可通过阴极电弧沉积工序或者通过物理气相沉积(PVD)工序,通过高功率脉冲磁控溅镀(HiPIMS)的方法涂覆。A further object of the present invention is to provide a piston ring comprising a substrate provided with a coating consisting of a metal nitride, which can be deposited by a cathodic arc deposition process or by physical vapor deposition (PVD ) process, coated by the method of high power pulse magnetron sputtering (HiPIMS).

发明的简要描述brief description of the invention

本发明的目的通过用于内燃机的、设置有基本上环形的铁合金的基体的活塞环实现,所述基体上涂覆有包括第一结合层和至少第一或第二外层的涂层,所述第一和第二外层沉积在第一结合层上,多个相继沉积的第一和第二外层达到最大100微米的厚度,第一外层由掺杂的金属化学元素(x)的氮化物组成,掺杂的元素为铝(Al),第二外层由金属化学元素(x)的氮化物组成,第一外层设置有至少大于第二外层的厚度的一倍且小于第二外层的厚度的十倍的厚度。The object of the invention is achieved by a piston ring for an internal combustion engine provided with a substantially annular ferrous alloy substrate coated with a coating comprising a first bonding layer and at least a first or a second outer layer, so The first and second outer layers are deposited on the first bonding layer, a plurality of successively deposited first and second outer layers reaching a thickness of at most 100 micrometers, the first outer layer being composed of a doped metal chemical element (x) The doped element is aluminum (Al), the second outer layer is composed of the nitride of the metal chemical element (x), and the first outer layer is provided with a thickness at least greater than twice the thickness of the second outer layer and less than the thickness of the second outer layer. Two times the thickness of the outer layer.

本发明的目的还通过包括从铬(Cr)或者钛(Ti)或者铌(Nb)中选择的金属化学元素(x)的活塞环实现,第一和第二外层设置有1和200纳米之间的厚度,涂层包括沉积在第一结合层上的第二结合层,第一结合层由铬(Cr)或者铬/铝(CrAl)组成,而第二结合层由掺杂的氮化铬组成,掺杂的元素为铝(CrAlN)或者氮化铬(CrN),涂层由第一和第二结合层以及第一和第二外层组成,呈现出1800和2500HV(维氏硬度)之间的硬度,3%至6%的孔隙率以及200和700MPa(兆帕)之间的内应力。The object of the present invention is also achieved by a piston ring comprising a metallochemical element (x) selected from chromium (Cr) or titanium (Ti) or niobium (Nb), the first and second outer layers being provided with a distance between 1 and 200 nanometers The coating includes a second bonding layer deposited on the first bonding layer, the first bonding layer consists of chromium (Cr) or chromium/aluminum (CrAl), and the second bonding layer consists of doped chromium nitride Composition, the doped element is aluminum (CrAlN) or chromium nitride (CrN), the coating is composed of the first and second bonding layer and the first and second outer layer, showing between 1800 and 2500HV (Vickers hardness) between 3% and 6% porosity and internal stress between 200 and 700MPa (megapascal).

本发明的目的额外地通过用于获得内燃机的活塞环的工序实现,涂层包括第一结合层,第二结合层,第一外层以及第二外层,涂层通过阴极电弧沉积工序沉积,或者通过物理气相沉积(PVD)工序沉积,通过高功率脉冲磁控溅镀(HiPIMS)的方法。The object of the invention is additionally achieved by a process for obtaining a piston ring for an internal combustion engine, the coating comprising a first bonding layer, a second bonding layer, a first outer layer and a second outer layer, the coating being deposited by a cathodic arc deposition process, Or deposited by physical vapor deposition (PVD) process, by high power pulsed magnetron sputtering (HiPIMS) method.

而且,本发明的目的通过包括至少一个如上所限定的活塞环的内燃机实现。Furthermore, the object of the invention is achieved by an internal combustion engine comprising at least one piston ring as defined above.

附图说明Description of drawings

基于在附图中体现的实施例的示例将更加详细地描述本发明,在附图中:The invention will be described in more detail based on an example of embodiment embodied in the accompanying drawings, in which:

图1示出了本发明的活塞环的上视图及其组成部分;Fig. 1 shows the top view of the piston ring of the present invention and its components;

图2示出了涂覆至本发明的活塞环的涂层的描绘;Figure 2 shows a depiction of the coating applied to the piston ring of the present invention;

图3示出了本发明的涂层的沉积的工序的结构描绘;Figure 3 shows a structural depiction of the sequence of deposition of the coating of the invention;

图4示出了本发明的工序的阶段的流程图;Figure 4 shows a flow diagram of the stages of the process of the present invention;

图5示出了用于现有技术的活塞环与本发明的活塞环之间的磨损评估的比较测试的图标描绘;Figure 5 shows a graphical depiction of a comparative test for wear evaluation between piston rings of the prior art and piston rings of the present invention;

图6示出了用于现有技术的活塞环与本发明的活塞环之间的已完成的磨损的评估的比较测试的图标描绘。Figure 6 shows a pictorial depiction of a comparative test for the evaluation of the wear performed between a piston ring of the prior art and a piston ring of the invention.

具体实施方式detailed description

本发明涉及用于内燃机的活塞环1,所述活塞环1设置有基本上环形的铁合金的基体2,所述基体2上涂覆有多层涂层4,所述多层涂层4包括第一结合层10和至少沉积在第一结合层10上的第一外层11或第二外层12,多个后续沉积的第一外层11和第二外层12的厚度最大可达100微米,从而由于涂层与基体的高粘和性、低内应力、高硬度以及低孔隙率而在活塞环1上提供出色的耐磨性。The invention relates to a piston ring 1 for an internal combustion engine, which is provided with a substantially annular base body 2 of a ferrous alloy, on which base body 2 is coated a multilayer coating 4 comprising a first A bonding layer 10 and at least a first outer layer 11 or a second outer layer 12 deposited on the first bonding layer 10, a plurality of subsequently deposited first outer layers 11 and second outer layers 12 having a thickness up to 100 microns , thereby providing excellent wear resistance on the piston ring 1 due to the high adhesion of the coating to the substrate, low internal stress, high hardness and low porosity.

为了本发明的恰当的理解,需要参照用于内燃机的活塞环1的使用以及参照用于在活塞环1上涂覆涂层4所使用的工序提供初始的说明。For a proper understanding of the invention, an initial description needs to be provided with reference to the use of a piston ring 1 for an internal combustion engine and to the procedure used for applying a coating 4 to a piston ring 1 .

以通常的方式,活塞环1为自膨胀元件,也就是说是具有高膨胀力、具有作为其目的的提升内燃机的燃烧室的气体密封、连通进行气缸的壁上的润滑油膜控制,并用作从活塞箱气缸传递热的元件的弹性元件。In the usual way, the piston ring 1 is a self-expanding element, that is to say a high expansion force, having as its purpose the gas sealing of the combustion chamber of the internal combustion engine, the communication of the lubricating oil film control on the walls of the cylinder, and its function as The elastic element of the heat transfer element of the piston box cylinder.

活塞环1在工作状态下经受可能的最有害的条件,这能够使其经受过早的磨损。在该磨损的主要原因中可提到的尤其是不足的润滑,在高负荷下工作的发动机在许多其他因素中通过磨损或划伤而将活塞环的表面暴露至磨损的恶劣的工序。The piston ring 1 is subjected to the most harmful conditions possible under operating conditions, which can subject it to premature wear. Insufficient lubrication may be mentioned among the main causes of this wear, engines operating at high loads expose the surfaces of the piston rings to a harsh process of wear, by wear or scuffing, among many other factors.

具有将磨损最小化并且延长活塞环1的使用寿命的目的,在外部工作表面通常使用包括比环1的材料硬和耐磨的材料的覆盖物或涂层。With the aim of minimizing wear and prolonging the service life of the piston ring 1, a covering or coating comprising a harder and wear-resistant material than that of the ring 1 is usually used on the outer working surface.

这些涂层通常通过离子涂覆工序沉积。在这些工序中,物理气相沉积(PVD)被广泛应用。These coatings are usually deposited by ion coating processes. Among these processes, physical vapor deposition (PVD) is widely used.

PVD工序是原子沉积,其中沉积材料被从处于原子或分子的固体源通过低压气体(等离子)在活塞环1的外部接触基体的方向上汽化,在表面上冷凝。基体的涂层的形成取决于汽化的材料和基体的材料,基体的状态,使用的能量(温度和离子撞击)和氛围(化学反应,反应沉积等)。The PVD process is atomic deposition in which the deposited material is vaporized from a solid source in atoms or molecules by a low-pressure gas (plasma) in the direction where the outside of the piston ring 1 contacts the substrate, condensing on the surface. The formation of a coating on a substrate depends on the vaporized material and the material of the substrate, the state of the substrate, the energy used (temperature and ion impact) and the atmosphere (chemical reaction, reactive deposition, etc.).

在这方面,本发明公开了包括涂层4的活塞环1,所述涂层4具有作为必要特征的多层构造,也就是说多层相继沉积到一定厚度从而提供出色的耐磨性。该涂层4优选但不强制由通过高功率脉冲磁控溅镀(HiPIMS)的方法的物理蒸发沉积(PVD)工序涂覆,并且也可以通过阴极电弧沉积工序涂覆。In this respect, the present invention discloses a piston ring 1 comprising a coating 4 having, as an essential feature, a multilayer construction, that is to say layers successively deposited to a certain thickness so as to provide excellent wear resistance. This coating 4 is preferably, but not necessarily, applied by a physical vapor deposition (PVD) process by the method of high-power pulsed magnetron sputtering (HiPIMS), and can also be applied by a cathodic arc deposition process.

本发明的活塞环1允许第一优选、但不强制的构造,其中环1设置有基本上环形的铁合金的基体2,在基体2上涂覆有涂层4,所述涂层4包括第一结合层10和至少沉积在第一结合层10上的第一外层11或第二外层12,多个后续沉积的第一外层11和第二外层12的厚度最大可达100微米(参见图1和图2)。The piston ring 1 of the invention allows a first preferred, but not mandatory, configuration in which the ring 1 is provided with a substantially annular base body 2 of iron alloy, on which base body 2 is coated with a coating 4 comprising a first The bonding layer 10 and at least the first outer layer 11 or the second outer layer 12 deposited on the first bonding layer 10, the thickness of the first outer layer 11 and the second outer layer 12 deposited subsequently can be up to 100 microns ( See Figures 1 and 2).

第一外层11由掺杂的金属化学元素(x)的氮化物组成,掺杂的元素为铝(Al),而第二外层12由金属化学元素(x)的氮化物组成。The first outer layer 11 consists of a doped nitride of a metallochemical element (x), the doped element being aluminum (Al), while the second outer layer 12 consists of a nitride of a metallochemical element (x).

金属化学元素(x)从铬(Cr)、钛(Ti)或者铌(Nb)中挑选。因此,第一外层11由掺杂的氮化铬(CrAlN)组成,而第二外层12由氮化铬(CrN)组成。以同样的方式,如果使用钛,则第一外层11由掺杂的氮化钛(TiAlN)组成,而第二外层12由氮化钛(TiN)组成。使用铌,则第一外层11由掺杂的氮化铌(NbAlN)组成,而第二外层12由氮化铌(NbN)组成。The metal chemical element (x) is selected from chromium (Cr), titanium (Ti) or niobium (Nb). Thus, the first outer layer 11 consists of doped chromium nitride (CrAlN), while the second outer layer 12 consists of chromium nitride (CrN). In the same way, if titanium is used, the first outer layer 11 consists of doped titanium nitride (TiAlN), while the second outer layer 12 consists of titanium nitride (TiN). With niobium, the first outer layer 11 consists of doped niobium nitride (NbAlN) and the second outer layer 12 consists of niobium nitride (NbN).

本发明的活塞环1的涂层4还包括沉积在第一结合层10上的第二结合层20的沉积。第一结合层10由铬(Cr)或者铬/铝(CrAl)组成,而第二结合层20由掺杂的氮化铬组成,掺杂的元素为铝(CrAlN)或者氮化铬(CrN)。The coating 4 of the piston ring 1 of the invention also includes the deposition of a second bonding layer 20 deposited on the first bonding layer 10 . The first bonding layer 10 consists of chromium (Cr) or chromium/aluminum (CrAl), while the second bonding layer 20 consists of doped chromium nitride, the doping element is aluminum (CrAlN) or chromium nitride (CrN) .

第一结合层10与第二结合层20,如它们的名字所指示的,在由软的铁材料组成的基体2与由硬材料组成的涂层4之间提供结合,进行从软材料向硬材料的过渡,确保涂层4与基体2的粘和性。应当注意的是,第二结合层20的沉积是可选的。在这种情况下,涂层4仅包括第一结合层10。The first bonding layer 10 and the second bonding layer 20, as their names indicate, provide a bond between the base 2 composed of a soft iron material and the coating 4 composed of a hard material, from the soft material to the hard iron. The transition of the material ensures the adhesion of the coating 4 to the substrate 2. It should be noted that the deposition of the second bonding layer 20 is optional. In this case, the coating 4 comprises only the first bonding layer 10 .

涂层4包括10微米和100微米之间的厚度,以便第一外层11与第二外层12设置有在纳米序列的范围上的厚度,为1纳米的厚度,可选为2纳米,可选为3纳米,可选为10纳米,可选为直到200纳米的任何尺寸变化。The coating 4 comprises a thickness between 10 micrometers and 100 micrometers, so that the first outer layer 11 and the second outer layer 12 are provided with a thickness in the range of nanometers, a thickness of 1 nanometer, optionally 2 nanometers, which can be Selected as 3 nm, optionally 10 nm, optionally any size variation up to 200 nm.

第一外层11设置有大于第二外层12的厚度的至少一倍,直至最大十倍的厚度,导致接下来的厚度表达式:1<XAlN/XN<10,也就是说第一外层11(XAlN)与第二外侧12(XN)的厚度之间的比率应大于1且小于10。The first outer layer 11 is provided with a thickness greater than at least one time, up to a maximum of ten times, the thickness of the second outer layer 12, resulting in the following thickness expression: 1<XAlN/XN<10, that is to say the first outer layer The ratio between the thickness of 11 (XAlN) and the second outer side 12 (XN) should be greater than 1 and less than 10.

从所描述的表达式,理解了第一外层11应具有超过第二外层12的厚度的厚度。该事实由于第一外层11包括提供低的或无氧化以及高延展性的掺杂的元素铝(Al)的事实而发生。这样的特性在铝(Al)上提供更大的弹性变形能力,以这种方式能够吸收应力并且增加耐磨性。以这种方式,由于更厚的涂层14的第一外层11由铝(Al)组成的事实,以外涂层11、12的形式出现的涂层4提供高耐磨性和低内应力。From the expressions described, it is understood that the first outer layer 11 should have a thickness exceeding the thickness of the second outer layer 12 . This fact occurs due to the fact that the first outer layer 11 comprises the element aluminum (Al) doped providing low or no oxidation and high ductility. Such properties provide greater elastic deformation capacity on aluminum (Al), in this way able to absorb stress and increase wear resistance. In this way, the coating 4 in the form of outer coatings 11 , 12 provides high wear resistance and low internal stress due to the fact that the first outer layer 11 of the thicker coating 14 consists of aluminum (Al).

此外,涂层4包括第一外层11和具有周期性地相继沉积的第二外层12,这可扩展至数千层,包括从第一外层11和第二外层12的两个沉积层,三个沉积层,四个沉积层,五个沉积层,六个沉积层,100个沉积层,500个沉积层,1000个沉积层等。涂层4的最终沉积层将会是第一外层11或第二外层12。Furthermore, the coating 4 comprises a first outer layer 11 and a second outer layer 12 with periodic successive depositions, which can be extended to thousands of layers, including two deposits from the first outer layer 11 and the second outer layer 12 layers, three layers, four layers, five layers, six layers, 100 layers, 500 layers, 1000 layers, etc. The final deposited layer of the coating 4 will be the first outer layer 11 or the second outer layer 12 .

通过本发明实现的主要技术效果基于这些层用作消灭涂层4中的裂缝的传播的界面或屏障的事实,以这种方式从与基体2脱离的方面增加了涂层4的阻抗。The main technical effect achieved by the invention is based on the fact that these layers act as interfaces or barriers that eliminate the propagation of cracks in the coating 4 , increasing in this way the resistance of the coating 4 from detachment from the substrate 2 .

在优选的构造中,本发明的PVD涂覆工序在真空反应器中进行,所述真空反应器包括阴极或者非平衡磁控溅镀的材料源(UMB)以及高功率脉冲磁控溅镀(HiPIMS),UMB与HiPIMS阴极同时对涂层材料的供给起作用。In a preferred configuration, the PVD coating process of the present invention is carried out in a vacuum reactor comprising a cathode or material source for unbalanced magnetron sputtering (UMB) and high power pulsed magnetron sputtering (HiPIMS ), UMB and HiPIMS cathode act on the supply of coating material simultaneously.

HiPIMS沉积工序利用存在于基本上增加使离子到达涂层4的生长所发生的金属基体2的能量(更大的速度)的现象,观测到涂层4的结构和组织上的可观的变型。The HiPIMS deposition process takes advantage of the phenomenon that exists to substantially increase the energy (greater velocity) that allows the ions to reach the metal substrate 2 where the growth of the coating 4 occurs, a considerable modification in the structure and organization of the coating 4 is observed.

在转变为氮化物之前,HiPIMS沉积工序还允许材料的离子化,即通常的金属(Cr、Ti、Mo、Nb、Al等)的离子化。对其而言,金属离子撞向涂层4的表面的高能量加速允许在涂层4的生长期间获得涂层4的松弛,无需损失其硬度。The HiPIMS deposition process also allows ionization of the material, ie the usual metals (Cr, Ti, Mo, Nb, Al, etc.), before conversion to nitride. For its part, the high-energy acceleration of the metal ions striking the surface of the coating 4 allows a relaxation of the coating 4 to be obtained during the growth of the coating 4 without losing its hardness.

作为形成涂层4的离子的高能量的自然后果,尤其是HiPIMS工序,发生涂层4的显著的密集化,导致孔隙率的降低以及在基体2上的离子的出色的粘和性。As a natural consequence of the high energy of the ions forming the coating 4 , especially the HiPIMS process, a significant densification of the coating 4 occurs, leading to a reduction in porosity and excellent adhesion of the ions on the substrate 2 .

而且,该工序允许另一个益处,为涂层4的生长免于液滴(小粒子)提供可能性。因此,用于涂层4的沉积的HiPIMS工序允许实现出色的摩擦特性,诸如耐磨性和抗脱离性。Moreover, this procedure allows another benefit, offering the possibility to grow the coating 4 free from droplets (small particles). Thus, the HiPIMS procedure for the deposition of coating 4 allows to achieve excellent tribological properties such as wear resistance and detachment resistance.

从图3能够看出本发明的PVD涂覆工序包括至少两个阴极,即,沉积铝化铬(CrAl)的UMB阴极,以及包括铬金属(Cr)的沉积、构造在涂层4的外层11、12的沉积中所需的交替的HiPIMS阴极。It can be seen from Fig. 3 that the PVD coating process of the present invention includes at least two cathodes, i.e., the UMB cathode for depositing chromium aluminide (CrAl), and the deposition of chromium metal (Cr), constructed in the outer layer of coating 4 Alternating HiPIMS cathodes required in the deposition of 11, 12.

在另一个可能的构造中,本发明的PVD工序包括三个阴极,即,沉积铝化铬(CrAl)的两个UMB阴极,以及执行铬金属(Cr)的沉积的HiPIMS阴极。In another possible configuration, the PVD process of the invention comprises three cathodes, namely two UMB cathodes depositing chromium aluminide (CrAl), and a HiPIMS cathode performing the deposition of chromium metal (Cr).

PVD工序还允许包括四个阴极的第三种可能的构造,即,两个UMB阴极,沉积铝化铬(CrAl)的HiPIMS阴极,以及执行铬金属(Cr)的沉积的第二个HiPIMS阴极。The PVD process also allows a third possible configuration comprising four cathodes, namely, two UMB cathodes, a HiPIMS cathode depositing chromium aluminide (CrAl), and a second HiPIMS cathode performing the deposition of chromium metal (Cr).

应当注意的是,真空反应器包含偶数或奇数数量的阴极,依据每个项目和需要,在一个、两个、三个、四个、五个、六个等之间选择阴极。It should be noted that the vacuum reactor contains an even or odd number of cathodes, choosing between one, two, three, four, five, six, etc., depending on each project and need.

以这种方式,本发明的涂覆工序允许以替换材料的纳米比例进行外层11、12的沉积,从而改善抗氧化特性,在工序参数的调整的同时导致低内应力,改善碎片的阻抗以及涂层的脱离。In this way, the coating process of the invention allows the deposition of the outer layers 11, 12 at a nanoscale ratio of the replacement material, thereby improving the oxidation resistance properties, leading to low internal stresses while adjusting the process parameters, improving the resistance of fragments and Detachment of the coating.

优选地,本发明的PVD工序包括设置有四个阴极的真空反应器,至少一个HiPIMS阴极,以及涂层4的涂覆的五个阶段(参见图4)。它们是:Preferably, the PVD process of the present invention comprises a vacuum reactor provided with four cathodes, at least one HiPIMS cathode, and five stages of application of the coating 4 (see FIG. 4 ). They are:

阶段1。对活塞环1进行化学清洁并安装在真空反应器中。在将活塞环1安装在反应器中之前,通过化学溶液对环1的基体2的表面进行清洁,将其表面的全部油质移除。Phase 1. Piston ring 1 is chemically cleaned and installed in a vacuum reactor. Before the piston ring 1 is installed in the reactor, the surface of the base body 2 of the ring 1 is cleaned with a chemical solution to remove all oil on the surface.

阶段2。反应器的撞击和加热。为了防止任何的污染,活塞环1必须被除气。阶段2包括在低于0.00007mbar(毫巴)下持续90分钟的达到400摄氏度的温度。Phase 2. Reactor impingement and heating. To prevent any contamination, the piston ring 1 must be degassed. Phase 2 includes a temperature of up to 400 degrees Celsius at less than 0.00007 mbar (mbar) for 90 minutes.

阶段3。由HiPIMS阴极提供的活塞环1的离子酸洗,以清洁基体2的表面。涂覆等离子与基体2的表面之间的偏电压在待涂覆的表面上提供铬(Cr+)的撞击,这样的工序通过表面的溅镀提供。阶段3发生在纯氩气以及5rpm(转每分钟)的恒转速,达到400摄氏度的温度,0.001mbar(毫巴)的压力,5.5kW(千瓦)和100Hz(赫兹)的铬的脉冲频率,-0.1V(伏特)的偏电压以及30分钟的持续时间的氛围下。Phase 3. Ionic pickling of the piston ring 1 provided by the HiPIMS cathode to clean the surface of the substrate 2. The bias voltage between the coating plasma and the surface of the substrate 2 provides an impact of chromium (Cr + ) on the surface to be coated, such a process being provided by sputtering of the surface. Phase 3 takes place in pure argon at a constant speed of 5 rpm (revolutions per minute), reaching a temperature of 400 degrees Celsius, a pressure of 0.001 mbar (mbar), a pulse frequency of 5.5 kW (kilowatts) and 100 Hz (hertz) of chromium, - Under a bias voltage of 0.1V (volts) and a duration of 30 minutes.

阶段4。设置在活塞环1的基体2上的多层涂层4的涂覆。铝化铬(CrAl)和铬(Cr)阴极交替定位,在环1的基体2的外表面上沉积三重材料(CrAlN),第一外层11、以及二元材料(CrN),第二外层12。应当注意的是,铬(Cr+)负责沉积在表面上的涂层4的离子撞击,缓解涂层4的应力。stage 4. Application of the multilayer coating 4 arranged on the base body 2 of the piston ring 1 . Chromium aluminide (CrAl) and chromium (Cr) cathodes are positioned alternately, on the outer surface of the base 2 of the ring 1 is deposited a triple material (CrAlN), a first outer layer 11, and a binary material (CrN), a second outer layer 12. It should be noted that chromium (Cr + ) is responsible for the ion impact of the coating 4 deposited on the surface, relieving the stress of the coating 4 .

可替代地,能够仅包括沉积在第一结合层10(Cr)上的第二结合层20(CrAlN)而执行阶段4,第二结合层20用作外层11、12的涂覆的支撑层。在该构造中,第二结合层20通过氮化铬(CrN)的阴极溅镀。Alternatively, stage 4 can be performed comprising only a second bonding layer 20 (CrAlN) deposited on a first bonding layer 10 (Cr), the second bonding layer 20 serving as a support layer for the coating of the outer layers 11, 12 . In this configuration, the second bonding layer 20 is sputtered by chromium nitride (CrN).

阶段4发生在包括在400摄氏度与420摄氏度之间的温度的50%的氩气和氮气的混合物和0.0022mbar(毫巴)的压力的氛围中。UBM阴极使用8.0kW(千瓦)和23.0Hz(赫兹)的脉冲频率沉积铝化铬(CrAl),第一HiPIMS阴极使用8.0kW(千瓦)和400Hz(赫兹)的频率沉积铬(Cr),而第二HiPIMS阴极使用8.0kW(千瓦)和400Hz(赫兹)的频率沉积铝化铬(CrAl)。阶段4还通过-65V(伏特)的偏电压发生,并且具有600分钟的平均持续时间,根据所沉积的涂层4的最终厚度变化。Stage 4 takes place in an atmosphere comprising a 50% mixture of argon and nitrogen at a temperature between 400 and 420 degrees Celsius and a pressure of 0.0022 mbar (mbar). The UBM cathode uses 8.0kW (kilowatt) and 23.0Hz (Hz) pulse frequency to deposit chromium aluminide (CrAl), the first HiPIMS cathode uses 8.0kW (kilowatt) and 400Hz (hertz) to deposit chromium (Cr), and the second Two HiPIMS cathodes deposit chromium aluminide (CrAl) using 8.0 kW (kilowatts) and 400 Hz (hertz). Phase 4 also takes place with a bias voltage of -65V (volts) and has an average duration of 600 minutes, varying according to the final thickness of the deposited coating 4 .

阶段5。对活塞环1进行冷却和卸荷。在完成涂层4的涂覆后,活塞环1被保持在真空反应器内以便系统冷却至100摄氏度以下,然后移去环1并使用待涂覆的新环1重新开始涂覆工序。阶段5初始处于420摄氏度的温度直到达到环境温度,处于对大气压力0.0022mbar(毫巴)的压力,持续90分钟。stage 5. Cool and unload piston ring 1. After finishing the application of the coating 4, the piston rings 1 were kept in the vacuum reactor so that the system cooled down to below 100 degrees Celsius, and then the rings 1 were removed and the coating process was restarted with new rings 1 to be coated. Stage 5 was initially at a temperature of 420 degrees Celsius until ambient temperature was reached, at a pressure of 0.0022 mbar (mbar) to atmospheric pressure, for 90 minutes.

已经在发动机上进行测试以评估本发明的活塞环1的耐磨性以及涂层4与活塞环1的基体2的粘和性。测试在安装在高负荷柴油发动机中的本发明的三个活塞环1上以及安装在高速柴油发动机中的本发明的两个活塞环1上执行。Tests have been carried out on an engine to evaluate the wear resistance of the piston ring 1 of the invention and the adhesion of the coating 4 to the base body 2 of the piston ring 1 . The tests were carried out on three piston rings 1 of the invention installed in a high-load diesel engine and on two piston rings 1 of the invention installed in a high-speed diesel engine.

第一磨损评估测试在高负荷柴油发动机中执行,并且环1在测力计中被递送至加速的热冲击测试超过250小时,其中发动机的机体和气缸衬套的热变形的状态,除了油膜的破裂的恶劣状态,在环1的工作表面上尤其观察到。应当进一步注意的是,为了尽可能地最小化所涉及的变化,气缸衬套与活塞环1从相同的生产批次获得。The first wear evaluation test was performed in a high-load diesel engine, and the ring 1 was delivered to an accelerated thermal shock test in a dynamometer for more than 250 hours, in which the state of thermal deformation of the engine block and cylinder liners, except for the oil film A bad state of cracking, especially observed on the working surface of the ring 1 . It should be further noted that, in order to minimize the variations involved as much as possible, the cylinder liner is obtained from the same production batch as the piston ring 1 .

图5表现了上述对比磨损评估测试的图标结果,现有技术I为设置有包括由阴极电弧沉积的氮化铬(CrN)的单层涂层4,同时现有技术II包括与现有技术I的涂层类似的涂层4,但是通过高功率脉冲磁控溅镀(HiPIMS)沉积。Figure 5 presents the graphical results of the comparative wear evaluation tests described above, prior art I provided with a single layer coating 4 comprising chromium nitride (CrN) deposited by cathodic arc, while prior art II comprising The coating is similar to coating 4, but deposited by high power pulsed magnetron sputtering (HiPIMS).

图5的图标额外表现了在提供有多层涂层4的构造I下的本发明的活塞环1,所述多层涂层4包括通过阴极电弧沉积的掺杂有铝的铬(CrAlN)和氮化铬(CrN)的相继沉积的外层11、12;并且构造II包括与构造I的涂层类似的涂层4,然而通过高功率脉冲磁控溅镀(HiPIMS)沉积。The diagram of FIG. 5 additionally represents a piston ring 1 according to the invention in configuration I provided with a multilayer coating 4 comprising aluminum-doped chromium (CrAlN) deposited by cathodic arc deposition and successively deposited outer layers 11, 12 of chromium nitride (CrN); and configuration II comprising a coating 4 similar to that of configuration I, however deposited by high power pulsed magnetron sputtering (HiPIMS).

在现有技术I和II的活塞环1表现出大约4.0微米的磨损的基础上,从图5能够清楚地看出本发明的活塞环1相对于现有技术表现了最小的磨损,然而本发明的构造I和构造II分别表现出3.5微米和2.3微米的磨损。以这种方式,本发明的活塞环1的构造II相对于现有技术I和II表现出小于大约50%的磨损。对其而言,本发明的构造I虽然没有清楚地产生与本发明的构造II一样好的结果,但无论产生的满意的结构,对于在内燃机中的应用而言,相对于现有技术证明了大大的益处。On the basis that the piston rings 1 of the prior art I and II exhibit a wear of about 4.0 microns, it can be clearly seen from FIG. The configurations I and II exhibited wear of 3.5 microns and 2.3 microns, respectively. In this way, configuration II of the piston ring 1 of the invention exhibits less than approximately 50% wear relative to prior art I and II. For its part, configuration I according to the invention does not clearly produce as good a result as configuration II according to the invention, but whatever produces a satisfactory structure, for use in internal combustion engines, proves, relative to the prior art Great benefit.

第二测试在高速柴油机中执行了超过500小时,使用如现有技术II的设置有包括掺杂有钛的氮化钛(TiAlN)的多层涂层4的活塞环1和在构造II中的本发明的活塞环1。再一次,本发明的活塞环1产生出色的结果,揭露了2.3微米的磨损,同时现有技术III的环1表现出20.1微米的磨损。以这种方式,本发明的环1相比于现有技术III的环1(参见图6)表现出小于大约80%的磨损。The second test was carried out in a high-speed diesel engine for more than 500 hours, using a piston ring 1 provided with a multilayer coating 4 comprising titanium-doped titanium nitride (TiAlN) as prior art II and in configuration II Piston ring 1 of the present invention. Again, the inventive piston ring 1 produced excellent results, revealing a wear of 2.3 microns, while the prior art III ring 1 exhibited a wear of 20.1 microns. In this way, the ring 1 of the invention exhibits less than approximately 80% wear compared to the ring 1 of prior art III (see FIG. 6 ).

而且,现有技术I、II以及III的活塞环表现出涂层4从基体2的脱离,同时本发明的活塞环1确保了涂层4与基体2的粘和性。Furthermore, the piston rings of prior art I, II and III exhibit detachment of the coating 4 from the matrix 2 , while the piston ring 1 of the invention ensures adhesion of the coating 4 to the matrix 2 .

还需要注意的是,通过1800和2500HV(维氏硬度)之间的硬度和200和700MPa(兆帕斯卡)之间的内应力,优选300和600Mpa(兆帕斯卡)之间的内应力,本发明的活塞环1的涂层4表现出小于6%的孔隙率,优选表现出3%的孔隙率。It should also be noted that, through the hardness between 1800 and 2500HV (Vickers hardness) and the internal stress between 200 and 700MPa (megapascal), preferably between 300 and 600Mpa (megapascal), the present invention The coating 4 of the piston ring 1 exhibits a porosity of less than 6%, preferably a porosity of 3%.

本发明的PVD工序的具体布置,连同工序的参数和材料的选择允许获得具有达到60微米的厚度的涂层,不会损害涂层的结构和机械强度。The specific arrangement of the PVD process of the invention, together with the parameters of the process and the choice of materials, allows to obtain coatings with thicknesses up to 60 microns, without compromising the structure and mechanical strength of the coating.

本发明的活塞环1设置有具有高耐磨性、低应力的涂层4,以这种方式防止了大粒子或者结构的不连续的形成,导致对碎片的高阻抗以及防止涂层4从活塞环1的基体脱离。The piston ring 1 of the invention is provided with a coating 4 with high wear resistance and low stress, in this way prevents the formation of large particles or discontinuities of structures leading to a high resistance to debris and prevents the coating 4 from dislodging from the piston The matrix of ring 1 is detached.

已经描述了优选实施例的示例,应当理解的是,本发明的范围覆盖其他可能的变型,仅由所附的权利要求的内容限定,其中包括可能的等同替代方式。Having described an example of a preferred embodiment, it should be understood that the scope of the invention covers other possible modifications, being limited only by the content of the appended claims, including possible equivalents.

Claims (10)

1. the piston ring (1) for internal combustion engine, it is provided with substantially annular, the base of ferroalloy Body (2), is coated with the coating (4) including the first binder course (10), described ring (1) on the matrix It is characterized in that described coating (4) additionally includes:
At least one first outer layer (11) or one second outer layer (12), described first outer layer (11) and described Second outer layer (12) is deposited on described first binder course (10), described the first of multiple sequential deposition With the thickness that the second outer layer (11,12) reaches maximum 100 microns,
Described first outer layer (11) is made up of the nitride of the metallic chemical element (x) adulterated, described in mix Miscellaneous element is aluminum (Al),
Described second outer layer (12) is made up of the nitride of metallic chemical element (x),
Described first outer layer (11) is provided with a times of the thickness at least above described second outer layer (12) And the thickness of ten times of thickness less than described second outer layer (12).
2. piston ring (1) as claimed in claim 1, it is characterised in that described metallic chemical element (x) Select from chromium (Cr) or titanium (Ti) or niobium (Nb).
3. piston ring (1) as claimed in claim 1, it is characterised in that described first and second outer layers (11, 12) thickness between 1 to 200 nanometers it is provided with.
4. piston ring (1) as claimed in claim 1, it is characterised in that described coating (4) includes sinking Amass the second binder course (20) on described first binder course (10).
5. piston ring (1) as claimed in claim 4, it is characterised in that described first binder course (10) It is made up of chromium (Cr) or chromium/aluminum (CrAl), and described second binder course (20) is by the nitridation adulterated Chromium forms, and the element of described doping is aluminum (CrAlN) or chromium nitride (CrN).
6. piston ring (1) as claimed in claim 4, it is characterised in that described coating (4) is by described First and second binder courses (10,20) and described first and second outer layers (11,12) composition, in Reveal the hardness between 1800 and 2500HV (Vickers hardnesses).
7. piston ring (1) as claimed in claim 4, it is characterised in that described coating (4) is by described First and second binder courses (10,20) and described first and second outer layers (11,12) composition, in Reveal the porosity of 3% to 6%.
8. piston ring (1) as claimed in claim 4, it is characterised in that described coating (4) is by described First and second binder courses (10,20) and described first and second outer layers (11,12) composition, in Reveal the internal stress between 200 and 700MPa (MPa).
9. for obtaining an operation for the piston ring (1) for internal combustion engine as claimed in claim 1, It is characterized in that coating (4) includes the first binder course (10), the second binder course (20), the first outer layer (11) And second outer layer (12), deposited by cathodic arc deposition operation, or by physical vapour deposition (PVD) (PVD) Operation deposits, by the method for high power pulse magnetic control sputtering plating (HiPIMS).
10. an internal combustion engine, it is characterised in that it includes that at least one is lived as defined in claim 1 Plug ring (1).
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